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New Orbit Determination and Clock synchronisation modules for EGNOS

机译:用于EGNOS的新的轨道确定和时钟同步模块

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摘要

The purpose of a Satellite Based Augmentation System (SBAS), such as EGNOS or WAAS, is to identify all range error sources and to distribute the corresponding corrections to the civil aviation user community with reliable navigation services for different flight phases. The effect of a satellite location error depends on the user location while a satellite clock error with respect to a reference time scale directly translates into a common pseudorange error to all the users. Therefore the SBAS shall broadcast a 3D vector that represents the satellite orbit error and a satellite clock correction.udTo achieve this objective the SBAS shall internally estimate the orbits and clocks for all the navigation satellites in view of the service area. The orbit determination function is in charge of computing the satellite ephemerides. The synchronization function computes the corresponding clock bias for each epoch and each satellite. Then the corrections are constructed from the differences between these orbits and clocks and the corresponding ones broadcasted inside the GNSS navigation messages. udStarting from R&D activities, Thales Alenia Space has developed new orbit determination and synchronization modules that are part of the Thales Algorithm Navigation Chain. These modules have been designed in collaboration with the orbit determination team at CNES (the French Space Agency).udThe new proposed orbit determination module is based on real time processing using code carrier measurement only. This module provides a stable and metric GPS orbit performance using an SBAS set of receivers corresponding to the EGNOS service area. The new synchronization module solves clock errors directly steered to GPS reference time scale, for the stations and satellites. It uses both code carrier and phase carrier measurements as well as the orbits estimated by the orbit determination process. The clocks solution error Allan’s deviation is around 10-12 at 120s leading to 7cm of possible deviation for a prediction up to 120s. This performance is fully compatible with the needs of the SBAS mission.udThese modules are now fully integrated into the SPEED platform, the SBAS Operational Test-bed that fully represents EGNOS Performances in terms of accuracy, continuity, availability and integrity for Safety Of Life services. The performance evaluation shows a real improvement over the current EGNOS algorithms, particularly in terms of the distribution of the Satellite Residual Error for the Worst user location (SREW).udThis paper provides a high level architecture description of this new Thales solution. A set of performance figures showing the achieved improvements is also presented.
机译:诸如EGNOS或WAAS之类的基于卫星的增强系统(SBAS)的目的是识别所有范围误差源,并通过针对不同飞行阶段的可靠导航服务,将相应的更正分发给民航用户社区。卫星位置误差的影响取决于用户位置,而相对于参考时间标度的卫星时钟误差直接转换为所有用户的常见伪距误差。因此,SBAS将广播表示卫星轨道误差和卫星时钟校正的3D矢量。 ud为了实现此目标,SBAS应在服务区域内内部估计所有导航卫星的轨道和时钟。轨道确定功能负责计算卫星星历表。同步功能为每个时期和每个卫星计算相应的时钟偏差。然后,根据这些轨道和时钟与GNSS导航消息中广播的相应轨道和时钟之间的差异来构造校正。 ud从研发活动开始,Thales Alenia Space开发了新的轨道确定和同步模块,这些模块是Thales算法导航链的一部分。这些模块是与法国航天局(CNES)的轨道确定小组合作设计的。 ud新提议的轨道确定模块仅基于使用代码载波测量的实时处理。该模块使用与EGNOS服务区域相对应的SBAS接收器集来提供稳定和度量的GPS轨道性能。新的同步模块解决了站和卫星直接参考GPS参考时标的时钟误差。它使用代码载波和相位载波测量,以及轨道确定过程估计的轨道。时钟解误差Allan的偏差在120s时约为10-12,导致7cm的可能偏差,最长可预测120s。这些性能模块现已完全集成到SPEED平台即SBAS操作测试台中,该平台可在准确性,连续性,可用性和完整性方面全面体现EGNOS的性能,以保障生命安全服务。性能评估显示了对当前EGNOS算法的真正改进,特别是在最差用户位置(SREW)的卫星残留误差分布方面。 ud本文提供了此新Thales解决方案的高级体系结构描述。还提供了一组性能数据,显示了已实现的改进。

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